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2-person ULM aircraft B2-SS-582-NF
2-stroke engineinstructionalsingle-engine

2-person ULM aircraft
2-person ULM aircraft
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Characteristics

Number of seats
2-person
Motorization
2-stroke engine
Applications
instructional
Other characteristics
single-engine
Length

19'00"
(5.79 m)

Height

7'00"
(2.13 m)

Wingspan

31'00"
(9.45 m)

Wing surface

173 ft²

Empty weight

585 lb
(265 kg)

Max. take-off weight

1,320 lb
(599 kg)

Fuel capacity

16 gal

Cruise speed

50 mph, 55 mph, 70 mph
(80 km/h, 89 km/h, 113 km/h)

Never exceed speed

84 mph
(135 km/h)

Take-off distance required

165'00"
(50 m)

Landing distance required

300'00"
(91 m)

Description

rotax 582 Powerplant Engine with ”C” Gearbox, warp drive propeller, EIS Engine Information System, 15” Main gear tires with aluminum wheels and 6” Drum brakes, 13” Nose gear with aluminum wheel, Center mounted controls with brake handle, Large lord mounted anti-vibration engine mount, Steel pilot roll cage. Aerodynamic lift and iury struts with adjustable fittings, High lift airfoil with 14”rib spacing, Center hard-shell gap cover, Bungee trim system GENERAL SPECIFICATIONS Model RotaxS82 No. Cylinders2 Displacement580.5 CC Horsepower65 H.P. Recommended T.B.O.300 Hrs PropellerWD-ADJ Wing Loading7.63 lb/sq Seats2 PERFORMANCE Takeoff Distance, Ground Roll 165 ft Obstacle 425 ft Rate of Climb 625 fpm Max Level Speed, Sea Level 70 mph Obstacle 300 ft Landing Distance, Ground Roll 85 ft Minimum Sink Rate 675 fpm Glide Ratio 5.95 to 1

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*Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.